Boeing MD-11F

Service difficulty reports · 31,317

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'MD11F'
  ORDER BY difficulty_date DESC"

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SDR IPXA2020071317647Hinge Fitting · wornINSPECTION TYPE:3CRT WING O/B FLAP O/B FWD HINGE UPPER ACTUATOR I/B LUG BUSHING IS LOOSE.REPAIRED RT WING O/B FLAP O/B FWD HINGE UPPER ACTUATOR I/B LUG WORN BUSHING BORE IAW VT-SAA EA 011-5740-01-A8394 REV. IR AND UPS EO MD11-5740-77054-A. (MINOR)Jun 25, 2020 · N281UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020070657409Skin · corrodedINSPECTION TYPE:3C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)Jun 25, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020070657407Skin · corrodedINSPECTION TYPE:3C EXTERIOR FUSELAGE HAS CORROSION BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)Jun 25, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020070157190Bracket · chafedINSPECTION TYPE:SV NR 2 ENGINE BRIDGE ASSY BOX RIB 2ND FROM O/B ON RT SIDE HAS A CHAFED BOLT HOLE. REMOVED AND REPLACED NR 2 ENGINE BRIDGE ASSY BOX RIB 2ND FROM O/B IAW SRM 51-33-01. (MINOR)Jun 25, 2020 · N283UP · Doug MD11F · Engine Cowling SystemSDR IPXA2020062656974Skin · gougedINSPECTION TYPE:2C RT WING FIXED L/E SKIN UPPER SURFACE AT STA XOS 1170 GOUGED. REPAIRED GOUGED RT WING FIXED L/E SKIN AT STA XOS 1170 IAW EA 011-5730-01-A8370 I/R AND EO MD11-5730-76945-A. (MINOR)Jun 25, 2020 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020062656978Longeron · corrodedINSPECTION TYPE:2C CENTER CARGO LON 35R CORRODED AT STA 5-113. REPAIRED CORRODED CENTER CARGO LONGERON 35R BETWEEN STA Y=5-93-Y=5-123 IAW SRM 53-00-05, REPAIR1, FIG 201. (MAJOR)Jun 25, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202006251346Seat Track · damagedCABIN - SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1421 , X = - 47.5 . DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLAJun 25, 2020 · N605FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202006251345Seat Track · damagedCABIN - SEAT TRACK CROWN AREA FOUND DAMAGED AT LEFT HAND STATION 1289 , X = 47.5. DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENJun 25, 2020 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202006251344Seat Track · damagedCABIN - SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1421 , X = - 27.5 . DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACJun 25, 2020 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202006251343Fitting · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP STATION 2164 AND FOUND CRACK INDICATION. FOUND THE BANJO FITTING CRACKED APPROXIMATE 1/4" TRIMMED AS PER SRM 55-30-02-Jun 25, 2020 · N605FE · Doug MD11F · Vertical StabilizerSDR FDEA202006251342Floor Panel · damagedCABIN FLOOR PANEL 263EF TOP SURFACE DAMAGED AT CENTER STATION 1321 - 1361. DAMAGED FLOOR PANEL 263EF REMOVED AS PER AMM 53-21-04. FLOOR PANEL 263EF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-04. REPAIJun 25, 2020 · N605FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202006241324Lamp · inoperativeMDIS 523 25-60 7757. 24JUN20 SEA OPEN U. L1 DOOR REMOTE PRESSURE INDICATOR INOPERABLE. MEL 24JUN20 02:34 SEA U. RELEASED FOR SERVICE, PER MEL: 25-61-02 CATEGORY: C EXPIRATION: 04JUL20. "MEL 25-61-02: L1 DOOR EVAC SLIDE REMOTE PRESS INDICATOR INOPERABLE. Jun 24, 2020 · N523FE · Doug MD11F · Emergency EquipmentSDR IPXA2020071457781Stringer · crackedINSPECTION TYPE:3C CENTER WING TANK STRINGER 52 IS CRACKED AT STA XCW=46.5. REPAIRED CRACKED CENTER WING TANK STRINGER 52 BETWEEN STA XCW= 36 TO XCW= 58 IAW SRM 57-10-03 REPAIR 1 FIG 201. (MAJOR)Jun 24, 2020 · N281UP · Doug MD11F · Wing, Longeron/StringerSDR FDEA2020071041328Floor Panel · delaminatedCABIN - FLOOR PANEL #232EF TOP SURFACE FOUND DAMAGED AT RIGHT HAND STATION 495 - STATION 595 AND BETWEEN X= -75.5 TO X= -107.5 DAMAGED FLOOR PANEL #232EF AT CABIN RIGHT HAND STATION 495 - STATION 595 AND BETWEEN X= -75.5 TO X= -107.5 REMOVED AS PER AMM 53-Jun 24, 2020 · N605FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2020071041327Bracket · wornRIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN. WORN BUSHING AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE REMOVED AS PER MD-11 CMM20-10-7 AND FOUND LUG HOLE WITHIN LIMIT AS Jun 24, 2020 · N617FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020071041326Bracket · wornLEFT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN. WORN BUSHING PIVOT BORE REMOVED IAW CMM 20-10-7 AND FOUND LUG HOLE WITHIN LIMIT IAW CMM57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-Jun 24, 2020 · N617FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2020070157197Channel · damagedINSPECTION TYPE:SV NR 2 ENG, PYLON FAN COWL LANDING HAT CHANNEL IS DAMAGED. REPAIRED NR 2 PYLON FAN COWL LANDING HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)Jun 24, 2020 · N283UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2020070157196Channel · damagedINSPECTION TYPE:SV LT FAN COWL LANGING FRAME IS DAMAGED(MID-SPAN). REPAIRED FAN COWL FRAME IAW SRM 54-00-00 FIG 208. (MINOR)Jun 24, 2020 · N283UP · Doug MD11F · Engine Cowling SystemSDR IPXA2020070157195Channel · damagedINSPECTION TYPE:SV NR 2 PYLON RT FAN COWL LANDING HAT CHANNEL IS DAMAGED. REPAIRED DAMAGED HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)Jun 24, 2020 · N283UP · Doug MD11F · Engine Cowling SystemSDR IPXA2020070157226Channel · damagedINSPECTION TYPE:SV NR 2 ENG LT FAN COWL SKIN PANEL LANDING HAT CHANNEL IS DAMAGED. REPAIRED HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)Jun 24, 2020 · N283UP · Doug MD11F · Engine Cowling SystemSDR IPXA2020070157188Skin · chafedINSPECTION TYPE:SV NR 2 LT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IS CHAFED THROUGH. REMOVED AND REPLACED CHAFED NR 2 LT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IAW SRM 51-35-01. (MINOR)Jun 24, 2020 · N283UP · Doug MD11F · Engine Cowling SystemSDR IPXA2020070157187Skin · chafedINSPECTION TYPE:SV NR 2 RT FAN COWL CLOSE OUT SKIN (DOOR JAMB) SKIN IS CHAFED THROUGH. REMOVED AND REPLACED CHAFED NR 2 RT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IAW SRM 51-35-01. (MINOR)Jun 24, 2020 · N283UP · Doug MD11F · Engine Cowling SystemSDR FDEA2020062541325Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09 AND FOUND EXCEED LIMIT BASEDJun 24, 2020 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2020062541328Floor Panel · delaminatedCABIN FLOOR PANEL 232EF FOUND DAMAGED AT RH BS 495- 595.Jun 24, 2020 · N605FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2020062541327Hinge · wornRIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN.Jun 24, 2020 · N617FE · Doug MD11F · Wing, Attach FittingsSDR FDEA2020062541326Hinge · wornLEFT HAND WING-INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN.Jun 24, 2020 · N617FE · Doug MD11F · Wing, Attach FittingsSDR FDEA2020062541324Indicator · inoperativeL1 DOOR REMOTE PRESSURE INDICATOR INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY. IDENTIFIED PARTS INDICATOR LAMP ASSY.Jun 24, 2020 · N523FE · Doug MD11F · Escape SlideSDR IPXA2020072087913Stringer · crackedINSPECTION TYPE:3C, LEFT WING NR 1 MAIN FUEL TANK UPPER STRINGER 6 AT XORS 316.9 WAS CRACKED. REPAIRED THE LT WING FUEL TANK UPPER STRINGER 6 IAW 011-5710-01-A8398, REV IR AND EO MD11-5710-77236-A. (MAJOR)Jun 23, 2020 · N281UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2020071457784Support Channel · corrodedINSPECTION TYPE:3C LT AFT FUSELAGE TO HORIZ STAB FAIRING SUPPORT CHANNEL IS CORRODED. REMOVED, FABRICATED AND REPLACED CHANNEL IAW DWG AJC7898 AND SRM 51-31-00. (MINOR)Jun 23, 2020 · N281UP · Doug MD11F · Fuselage, Stabilizer Attach FittingsSDR IPXA2020071457779Stringer · crackedINSPECTION TYPE:3C LT WING STRINGER 5 IS CRACKED BETWEEN STA XORS= 683.4 TO 700.0 AND BETWEEN STA XORS= 713.65 TO 737.55. REPAIRED CRACKED LT WING STRINGER 5 BETWEEN STA XORS= 669 TO 700 AND BETWEEN STA XORS= 726 TO 757 IAW SRM 57-00-00 REPAIR 3 FIG 201. (MAJJun 23, 2020 · N281UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2020071307624Support · chafedINSPECTION TYPE:3CL/H AFT FUSELAGE TO HORZ. STAB FAIRING SUPPORT FOR PANEL 337BF IS CHAFED.REPAIRED FAIRING SUPPORT IAW SRM SRM 55-00-00 PARA. 4 FIG. 208. (MINOR)Jun 23, 2020 · N281UP · Doug MD11F · Horizontal Stabilizer StructureSDR IPXA2020071097567Skin · corrodedINSPECTION TYPE:3CCENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -87.7 ABOVE STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= -87.7 ABOVE STR. 15 IAW VT-SAA EA 011-5730-01-A8388 REV. I/R AND UPS EO MD11-5730-77106-A. (MINOR)Jun 23, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020070157186Angle · crackedINSPECTION TYPE:SV LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ANGLE CRACKS. REMOVED AND REPLACED CRACKED LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL IAW EA 011-5530-01-A8380 REV IR AND EO MD11-5530-77008-A. (MAJOR)Jun 23, 2020 · N283UP · Doug MD11F · Vertical Stabilizer Miscellaneous StructureSDR FDEA202006231316Fan · failedON DESCENT INTO KOAK PASSING THROUGH APPROX FL280 STARTED SMELLING AN ACRID SMELL ACCOMPANIED BY A RUMBLING SOUND. THE FO SAID HE FELT VIBRATIONS UNDER HIS FEET. THE SMELL INCREASED, SO WE DECLARED AN EMERGENCY. AS WE GOT BELOW 10,000FT AND THE PLANE DEPREJun 23, 2020 · N582FE · Doug MD11F · Air Distribution FanSDR FDEA202006231314Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 878 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 23, 2020 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202006231313Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 751 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 23, 2020 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202006231312Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 766 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 23, 2020 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202006231311Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 624 FOUND CRACK. LEFT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 624 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 23, 2020 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202006231310Former · crackedLEFT HAND WING LEADING EDGE CAVITY FORMER AT STATION XOS = 733 FOUND CRACK. CRACKED FORMER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW FORMER IAW DRAWING ARB2923, REVISION D. INSTALLED THE NEW FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IJun 23, 2020 · N605FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020071757821Longeron · corrodedINSPECTION TYPE: 3C, CENTER CARGO LONGERON 43L WAS CORRODED BETWEEN BS 1821 - 1841. REPAIRED THE LONGERON IAW EA 011-5310-01-A8387, REV I/R AND EO MD11-5310-77194-A. MAJOR.Jun 22, 2020 · N281UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020071317645Fuel Tank · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION ABOVE STRINGER 15 AT XCW=108.REPAIRED CENTER WING TANK UPPER SKIN CORROSION ABOVE STRINGER 15 AT XCW=108 IAW VT-SAA EA 011-5730-01-A8396 REV. IR AND UPS EO MD11-5730-77067-A. (MINOR)Jun 22, 2020 · N281UP · Doug MD11F · Fuel StorageSDR IPXA2020071317644Fuel Tank · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION ABOVE STRINGER 16 AT XCW=-101.REPAIRED CENTER WING TANK UPPER SKIN CORROSION ABOVE STRINGER 16 AT XCW=-101 IAW VT-SAA EA 011-5730-01-A8395 REV. IR AND UPS EO MD11-5730-77104-A. (MINOR)Jun 22, 2020 · N281UP · Doug MD11F · Fuel StorageSDR IPXA2020071097568Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -11 ABOVE STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= -11 ABOVE STR. 15 IAW VT-SAA EA 011-5730-01-A8391 REV I/R, AND EO MD11-5730-77097-A. (MINOR)Jun 22, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020071097565Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 55.5 AT STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 55.5 AT STR. 15 IAW VT-SAA EA 011-5730-01-A8393 REV. I/R AND UPS EO MD11-5730-77095-A. (MINOR)Jun 22, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020071097563Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 47 AND STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 47 AND STR. 15 IAW VT-SAA EA 011-5730-01-A8386 REV. I/R AND UPS EO MD11-5730-77099-A. (MINOR)Jun 22, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020071097562Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 2 AND STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 2 AND STR. 15 IAW VT-SAA EA 011-5710-01-A8392 REV. I/R AND UPS EO MD11-5730-77090-A. (MINOR)Jun 22, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020071097561Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -111 AT STR. 12.REPAIRED CENTER WING BOX UPPER SKIN AT STA. XCW= -111 AT STR. 12 IAW EA 011-5710-01-A8390 REV. I/R AND EO MD11-5730-770859-A. (MINOR)Jun 22, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020071097560Structure · corrodedINSPECTION TYPE:3C, LEFT WING SPOILER SILL IS CORRODED BETWEEN STA. XOSP= 494.50 TO XOSP= 566.75.REPAIRED CORRODED L/H WING SPOILER SILL BETWEEN STA. XOSP= 494.50 TO XOSP= 566.75 IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)Jun 21, 2020 · N281UP · Doug MD11F · SpoilersSDR FDEA2020070821302Floor Panel · damagedMAIN DECK CARGO COMPARTMENT AFT LEFT AREA , STATION Y1901 FLOOR PANEL #291GF (SECOND FROM OUTBOARD) FOUND SPONGY. MAIN DECK CARGO COMPARTMENT AFT LEFT AREA, X = 47.5 STATION Y1901. FLOOR PANEL #291GF REMOVED PER AMM 53-21-09-4, FABRICATED PER DRAWING SRJun 21, 2020 · N617FE · Doug MD11F · Fuselage Floor PanelSDR FDEA2020070821301Floor Panel · damagedMAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535 , OUTBOARD FLOOR PANEL #231EF FOUND WITH SEVERAL PUNCTURES. MAIN DECK CARGO COMPARTMENT LEFT SIDE X = 78 STATION Y535, OUTBOARD FLOOR PANEL #231EF REMOVED PER AMM 53-21-09-4, FABRICATED PER FEDEX DRAWINGJun 21, 2020 · N617FE · Doug MD11F · Fuselage Floor Panel
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